US8327604B2 - Mini-truss thin-sheet panel assembly - Google Patents
Mini-truss thin-sheet panel assembly Download PDFInfo
- Publication number
- US8327604B2 US8327604B2 US12/254,795 US25479508A US8327604B2 US 8327604 B2 US8327604 B2 US 8327604B2 US 25479508 A US25479508 A US 25479508A US 8327604 B2 US8327604 B2 US 8327604B2
- Authority
- US
- United States
- Prior art keywords
- sheet
- thin
- backer
- panel assembly
- assembly according
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related, expires
Links
- 239000000853 adhesive Substances 0.000 claims description 52
- 230000001070 adhesive effect Effects 0.000 claims description 52
- 239000011521 glass Substances 0.000 claims description 31
- 239000000463 material Substances 0.000 claims description 20
- 239000000835 fiber Substances 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 8
- 238000007493 shaping process Methods 0.000 claims description 7
- 239000000758 substrate Substances 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 230000006835 compression Effects 0.000 claims description 4
- 238000007906 compression Methods 0.000 claims description 4
- 238000010248 power generation Methods 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims description 4
- 238000009825 accumulation Methods 0.000 claims description 3
- 239000012141 concentrate Substances 0.000 claims description 3
- 230000005670 electromagnetic radiation Effects 0.000 claims description 3
- 230000006872 improvement Effects 0.000 claims description 2
- 229920003002 synthetic resin Polymers 0.000 claims description 2
- 239000000057 synthetic resin Substances 0.000 claims description 2
- 239000010409 thin film Substances 0.000 description 6
- 238000005452 bending Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000007767 bonding agent Substances 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 239000011152 fibreglass Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001413 cellular effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229920006332 epoxy adhesive Polymers 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 235000012773 waffles Nutrition 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/18—Handling of layers or the laminate
- B32B38/1866—Handling of layers or the laminate conforming the layers or laminate to a convex or concave profile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
- F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
- F24S23/74—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with trough-shaped or cylindro-parabolic reflective surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
- F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
- F24S23/74—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with trough-shaped or cylindro-parabolic reflective surfaces
- F24S23/745—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with trough-shaped or cylindro-parabolic reflective surfaces flexible
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
- F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
- F24S23/82—Arrangements for concentrating solar-rays for solar heat collectors with reflectors characterised by the material or the construction of the reflector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
- F24S25/40—Arrangement of stationary mountings or supports for solar heat collector modules using plate-like mounting elements, e.g. profiled or corrugated plates; Plate-like module frames
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
- H01L31/0547—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
- Y02E10/47—Mountings or tracking
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/52—PV systems with concentrators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
Definitions
- the present invention relates generally to a thin-sheet panel assembly, and more particularly to a mini-truss thin-sheet panel assembly adapted for use in solar collector applications.
- Solar collection facilities utilize solar concentrators and/or photovoltaic panels for harnessing solar energy.
- Solar concentrator assemblies SCAs
- movable parabolic trough collectors present large reflective surface areas (apertures) for tracking the sun and focusing the captured radiant energy on linear heat collection elements (HCEs) as a first step in a thermomechanical conversion process for generating electrical power.
- a solar-trough solar power generation facility typically includes many SCAs arranged in rows to capture great amounts of solar radiant energy.
- the reflective surfaces of troughs of SCAs are usually hot-formed, thick-glass mirrors that ideally conform to a given geometry, notably surface curvature.
- Operating efficiency of the solar plant is largely dependant on the ability of the mirrors to maintain surface curvature accuracy so that the mirrors sharply focus reflected sunlight on the HCE.
- This requires very exacting manufacturing processes for mirror production and high rigidity of the mirrors themselves as mounted to their supports.
- the glass is typically formed thicker, often resulting in a mirror weight that rivals the weight of the supporting structure.
- hot-formed, glass mirrors are used in various solar concentrating applications, such as the Nevada Solar One solar power generating plant in Nevada.
- the glass mirror material is hot-formed to the mathematical shape (surface geometry) required to reflect and concentrate sunlight on an HCE.
- Such hot-formed glass is also known as sagged glass. Sagged glass is thick, heavy, costly to manufacture, costly to transport and install at a facility, and prone to breakage.
- the thick glass mirrors must retain their mathematical shape in order to efficiently focus concentrated sunlight, which requires the hot-formed mirror glass to have a sufficient thickness to maintain the mirror shape (usually about three to five millimeters).
- Problems with the hot-formed glass include that the thicker glass reduces the reflective efficiency of the mirror (more absorption and less reflection of sunlight), has fabrication-related surface error limitations (slope error and edge effects), is more costly due to the increased amount of glass material, and is heavier resulting in undesirable shipping and handling issues.
- thick sheet material is difficult to form in the complex shapes needed for solar power applications and may trap water in the interface which corrodes the silvering.
- thin-glass and thin-film have been bonded directly against a pre-formed substrate or aluminum plate having a desired curvature, or to a sandwich panel made with the required surface geometry.
- Sandwich panels are usually comprised of two sheet metal surfaces bonded to a cellular core such as a honeycomb configuration.
- Historical problems with thin-glass and thin-film bonded directly against a pre-formed curved substrate or plate, or in combination with honeycomb and other types of closed-cell panel construction, are high cost and their affinity for water intrusion when exposed to weather. Trapped water attacks the preferably aluminum components and penetrates the mirror coatings, causing the mirror silvering to corrode.
- aspects of embodiments of the present invention are directed to a mini-truss thin-sheet panel assembly.
- the “mini-truss” design of a backing material element is important to providing rigidity to the mini-truss thin-sheet panel assembly.
- Embodiments of the mini-truss thin-sheet panel assembly maintain a thin panel, such as a thin sheet of glass or other reflective material, in a rigid or substantially rigid configuration.
- embodiments of the mini-truss thin-sheet panel assembly of the present invention may be utilized in solar collector troughs of a solar concentrator assembly (SCA), for example.
- SCA solar concentrator assembly
- a thin-glass panel of a mini-truss thin-sheet panel assembly may have about one fourth of the thickness and weight of sagged glass, and may be manufactured in a flat configuration without hot-forming (but may later be “cold formed” to a desired shape or curvature) and, therefore, may be manufactured at less cost.
- Another aspect of embodiments of the mini-truss thin-sheet panel assembly is the “cold” formability of the thin-glass or thin-film.
- Yet another aspect of embodiments of the mini-truss thin-sheet panel assembly is greater overall mirror rigidity and, therefore, improved accuracy as utilized in an SCA, for example. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is increased ease of installation. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is reduced transportation costs. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is elimination or reduction of secondary breakage, such as may result from heavy wind forces applied against thick-glass structures. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is interchangeability with or use in combination with existing solar troughs or other devices. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is improved reflective performance. Still another aspect of embodiments of the mini-truss thin-sheet panel assembly is a substantially open architecture for allowing moisture to drain or evaporate and thereby prevent or deter the accumulation of moisture between components of the assembly.
- a substantially rigid thin-sheet panel assembly having a non-rigid thin-sheet component includes the thin-sheet component which has selected plan area and shape, a backer having a plan shape and area substantially similar to the thin-sheet component, and plural riser elements of selected height and configuration each extending from the backer to distal ends connected to a reverse surface of the thin-sheet component, the riser elements being configured and disposed in an array which causes the assembly to have substantial rigidity in a selected direction in the thin-sheet component.
- the riser elements are of substantially uniform height from the backer so that the thin-sheet component and the backer have essentially concentric curvature.
- an obverse surface of the thin-sheet component has concave curvature.
- the concave curvature is parabolically cylindrical concave curvature.
- the selected direction is a circular direction substantially concentric to the center of area of the thin-sheet component. In one embodiment, the selected direction is at least one of two orthogonal directions in the thin-sheet component.
- the thin-sheet component includes a glass layer. In one embodiment, the thin-sheet component includes structural fibers for providing strength to the thin-sheet component.
- the backer is defined by a backer sheet
- the riser elements are defined by portions of the backer sheet that are bent away from the backer sheet and have integral connections to the backer sheet.
- the portions of the backer sheet that define the riser elements have substantially triangular configurations and the integral connections of the riser elements to the backer sheet are at bases of the triangular configurations.
- the integral connections of the riser elements to the backer sheet are spaced along substantially parallel lines, and the riser elements are in substantially parallel planes.
- the parallel planes are in first and second groups, the parallel planes in the first group being substantially normal to the parallel planes in the second group.
- the riser elements at their distal ends define connection tabs disposed laterally of the heights of the risers.
- the backer sheet includes aluminum.
- the backer is defined by a first backer sheet and a second backer sheet
- the riser elements are defined by portions of the first backer sheet that are bent away from and have integral connections to the first backer sheet and portions of the second backer sheet that are bent away from and have integral connections to the second backer sheet, the portions of the first and second backer sheets that define the riser elements having substantially triangular configurations, the integral connections to the first and second backer sheets at bases of the triangular configurations, the integral connections to the first backer sheet spaced along substantially first parallel lines, the integral connections to the second backer sheet spaced along substantially second parallel lines, the riser elements of the first backer sheet in substantially first parallel planes, the riser elements of the second backer sheet in substantially second parallel planes, the first parallel lines substantially normal to the second parallel lines, and the first parallel planes substantially normal to the second parallel planes.
- connections of the distal ends of the riser elements to the reverse surface of the thin-sheet component are bonded connections.
- the thin-sheet component includes a substrate layer composed principally of a selected synthetic resin material.
- the riser elements include apertures near the distal ends.
- the assembly defines a section of a larger parabolically curved cylindrical thin panel.
- the backer has a curvature different from a curvature of the thin-sheet component. In one embodiment, the curvature of the backer is substantially flat.
- the thin-sheet component is reflective of electromagnetic radiation. In one embodiment, the thin-sheet component is reflective of solar radiation.
- the thin-sheet panel assembly has a substantially open architecture configured to allow moisture to drain or evaporate therefrom and deter accumulation of moisture in the thin-sheet panel assembly.
- a support structure for supporting a thin panel to have a substantially rigid configuration includes a backer sheet, and a plurality of riser elements having heights extending in a first direction from proximal ends coupled to the backer sheet to distal ends and having lengths along rows in substantially parallel riser planes, the distal ends of the riser elements being attachable to the thin panel for supporting the thin panel and increasing rigidity of the thin panel in a second direction substantially parallel to the riser planes.
- an improvement including a substantially rigid thin-sheet panel assembly including: a non-rigid thin-sheet component having a first surface; a backer; and plural riser elements of selected height and configuration each extending from the backer to distal ends connected to a reverse surface of the thin-sheet component, the reverse surface opposite the first surface, the riser elements being configured and disposed in an array which causes the assembly to have substantial rigidity in a selected direction in the thin-sheet component, the first surface of the thin-sheet component including at least a portion of one of the plurality of curved reflective surfaces having the selected curvature.
- a method of forming a thin-sheet panel assembly having a thin-sheet component and a backer including a plurality of risers extending from the backer to distal ends includes: applying an adhesive to the distal ends of the risers; attaching the thin-sheet component to the distal ends of the risers via the adhesive; and shaping the thin-sheet panel assembly to have a selected curvature while the adhesive cures from an uncured state in which the adhesive does not adhere the thin-sheet component and the backer to one another to a cured state in which the adhesive adheres the thin-sheet component and the backer to one another.
- shaping the thin-sheet panel assembly includes: positioning the thin-sheet panel assembly between a first portion of a bonding fixture having a first curved surface and a second portion of the bonding fixture having a second curved surface, the first and second curved surfaces facing each other and substantially corresponding to the selected curvature; and clamping the first and second portions of the bonding fixture toward one another to restrain the thin-sheet panel assembly therebetween to have the selected curvature while the adhesive cures from the uncured state to the cured state.
- FIG. 1 is a front schematic view of a typical curved truss design
- FIG. 2 is a perspective schematic view of a solar concentrator assembly
- FIG. 3 is a top perspective view of a mini-truss thin-sheet panel assembly according to an embodiment of the present invention.
- FIG. 4 is a front view of the mini-truss thin-sheet panel assembly of FIG. 3 ;
- FIG. 5 is a bottom perspective view of the mini-truss thin-sheet panel assembly of FIG. 3 ;
- FIG. 6 is a detail bottom perspective view of a portion of the mini-truss thin-sheet panel assembly of FIG. 3 ;
- FIG. 7 is a top perspective view of a backer of the mini-truss thin-sheet panel assembly of FIG. 3 ;
- FIG. 8 is a top view of the backer of FIG. 7 ;
- FIG. 9 is a front view of the backer of FIG. 7 ;
- FIG. 10 is a detail top perspective view of a portion of the backer of FIG. 7 ;
- FIG. 11 is a detail top view of a portion of the backer of FIG. 7 ;
- FIG. 12 is a detail front view of a portion of the backer of FIG. 7 ;
- FIG. 13 is a top perspective view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 14 is a side view of the backer of FIG. 13 ;
- FIG. 15 is a top schematic view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 16 is a top schematic view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 17 is a top schematic view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 18 is a top schematic view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 19 is a top perspective view of a backer of a mini-truss thin-sheet panel assembly according to another embodiment of the present invention.
- FIG. 20 is a top perspective view of a bonding fixture for shaping a mini-truss thin-sheet panel assembly according to an embodiment of the present invention
- FIG. 21 is a front view of the bonding fixture of FIG. 20 ;
- FIG. 22 is a side perspective view of the bonding fixture of FIG. 20 ;
- FIG. 23 is a top perspective view of a first portion of the bonding fixture of FIG. 20 ;
- FIG. 24 is a top perspective view of a second portion of the bonding fixture of FIG. 20 ;
- FIG. 25 is a top perspective view of the bonding fixture of FIG. 20 in an open position
- FIG. 26 is a top perspective view of the bonding fixture of FIG. 20 , showing a mini-truss thin-sheet panel assembly on a first portion thereof;
- FIG. 27 is a top perspective view of the bonding fixture of FIG. 20 , showing a mini-truss thin-sheet panel assembly being shaped therein.
- mini-truss refers to an assembly of members forming a rigid, or substantially rigid, framework.
- a typical curved truss structure 10 includes an upper chord 12 , a lower chord 14 , and diagonal elements 16 , or lacing.
- the diagonal elements 16 extend between and connect the upper and lower chords 12 , 14 at various locations to provide strength and rigidity to the truss structure 10 .
- a solar concentrator assembly (“SCA”) 20 includes a row of parabolic, cylindrically curved, or otherwise curved, troughs 22 for collecting radiant solar energy.
- the troughs 22 have reflective surfaces for reflecting and focusing the radiant energy on a heat collection tube 25 .
- Each of the troughs 22 is supported by a corresponding trough frame 30 , which may be constructed of tubes, bars, extrusions, and/or any other suitable structural members for supporting and maintaining the critical shape of each of the troughs 22 and the reflective surfaces thereon.
- Each of the trough frames 30 may include two torque plates 35 , one on either side, for coupling to and supporting the trough frames 30 on supporting pylons 40 .
- the torque plates 35 may, for example, be coupled to the supporting pylons 40 at bearings 45 .
- a mini-truss thin-sheet panel assembly 100 includes a thin sheet 110 and a backer 120 that are attached to one another at various locations.
- the configuration of the mini-truss thin-sheet panel assembly 100 provides rigidity to the thin sheet 110 and also maintains the thin sheet 110 in a shape having a desired curvature.
- the reflective surfaces of the troughs 22 of the SCA 20 described above and shown in FIG. 2 , may be embodied as the mini-truss thin-sheet panel assembly 100 .
- the reflective surfaces of the troughs 22 will be configured to maintain a selected curvature for focusing solar radiation.
- the thin sheet 110 (upper chord), according to one embodiment, is a thin glass sheet.
- the thin sheet 110 is non-rigid and has a glass thickness of about one to two millimeters (about 0.04 to 0.08 inches).
- the thin sheet 110 may include glass of any other suitable thickness.
- other embodiments of the thin sheet 110 may be formed of any thin-gage, non-glass reflective material (see, e.g., U.S. Pat. No. 6,989,924 B1 and 2006/0181765 A1, and similar materials), such as a synthetic thin-film material, or a combination of materials, such as a thin-film on a flat sheet metal substrate.
- the thin sheet 110 may be formed of a thin-film material on a substrate having a thickness of about 0.5 to 1.5 millimeters (about 0.02 to 0.06 inches), or alternatively, any other suitable thickness.
- the thin sheet 110 may be formed of a material that is reflective of electromagnetic radiation, such as solar radiation. Further, in other alternative embodiments, the thin sheet 110 may be formed of one or more materials that are non-reflective, having a suitable thickness for the desired application. Further, as described further below, a thickness of the thin sheet 110 (upper chord) may be selected depending on a thickness of a backer sheet (lower chord) of the backer 120 .
- the thin sheet 110 may include a secondary structural element such as a thin layer of fiberglass, or similarly applied alternative suitable material, that provides relief for thin glass where tensile loads may become excessive.
- first structural fibers 112 may be bonded, or otherwise attached, to a bottom surface of the thin sheet 110 before the mini-truss thin-sheet panel assembly 100 is shaped to have a selected curvature.
- the first structural fibers 112 are attached to the thin sheet 110 having a direction that is substantially parallel to planes of risers of the backer 120 (see FIG. 3 ).
- second structural fibers 114 may be bonded, or otherwise attached, to a bottom surface of the thin sheet 110 before the mini-truss thin-sheet panel assembly 100 is shaped to have a selected curvature.
- the second structural fibers 114 are attached to the thin sheet 110 in a direction diagonal to the first structural fibers 112 (see FIG. 3 ).
- the second structural fibers 114 may be applied to the thin sheet 110 in substitution of, or in addition to, the first structural fibers 112 .
- the first and second structural fibers 112 , 114 provide strength to thin glass. Moreover, the first and second structural fibers 112 , 114 are bonded or otherwise applied to the thin sheet 110 before the mini-truss thin-sheet panel assembly 100 is shaped to have a selected curvature. As such, when the mini-truss thin-sheet panel assembly 100 is shaped to have a selected curvature, the first and second structural fibers 112 , 114 will be placed in tension, and the thin glass will thereby be placed in compression and remain in compression during use of the shaped mini-truss thin-sheet panel assembly 100 . This is beneficial because glass has optimal strength when in compression.
- the backer 120 includes a backer sheet 122 (lower chord).
- the backer sheet 122 is formed from aluminum sheet metal having a thickness of about 0.5 to 1.5 millimeters (about 0.02 to 0.06 inches).
- any other suitable material may be used to form the backer sheet 122 , including any other suitable sheet metal or other material having any suitable thickness.
- a thickness of the backer sheet 122 may be selected in cooperation with a thickness and structural characteristics of the thin sheet 110 so that, for example, the strengths of the thin sheet 110 (upper chord) and the backer sheet 122 (lower chord) are substantially balanced.
- the backer 120 further includes a plurality of risers 124 (diagonal elements).
- the risers 124 are arranged in multiple rows, and may be uniformly spaced in a grid or array pattern.
- Each of the risers 124 is integrally formed from the backer sheet 122 and has a substantially triangular-shaped configuration.
- the risers 124 may be formed by shearing, punching, cutting, water jet, or any other suitable device or method for separating the risers 124 from the backer sheet 122 , on two sides of the triangular shapes of the risers 124 . Further, in the embodiment shown, the risers 124 are folded away from the backer sheet 122 at a third side (i.e.
- the risers 124 have substantially uniform heights from the backer sheet 122 , which may be selected depending on thicknesses of the thin sheet 110 and the backer sheet 120 .
- the risers 124 may be folded, or bent, utilizing a progressive die or any other suitable device or apparatus, or alternatively may be folded by hand. When the risers 124 are folded and extend away from the backer sheet 122 , corresponding substantially triangular-shaped openings 125 remain in the backer sheet 122 .
- the rows of the risers 124 are in substantially parallel planes. That is, the fold lines of each of the risers 124 are spaced apart and substantially parallel to one another, and the risers 124 are in planes that are substantially parallel to one another. Further, the risers 124 are in planes that are substantially perpendicular to the backer sheet 122 . In an assembled embodiment of the mini-truss thin-sheet panel assembly 100 , the planes of the risers 124 are substantially perpendicular to an axis about which a curvature is formed in the mini-truss thin-sheet panel assembly 100 (see FIG. 4 ).
- the risers 124 will provide stiffness and rigidity to the mini-truss thin-sheet panel assembly 100 in a direction that will prevent or reduce any disruption from the selected curvature (e.g., by mirror deflections and/or thermal expansion and contraction), such as after installation at a solar facility.
- each of the risers 124 has an adhesive pad 130 (“connection tab”) protruding from the triangular shape at a distal end of each of the risers 124 .
- the adhesive pads 130 provide spaced apart regions of surface area for attaching the risers 124 to the thin sheet 110 .
- Each of the adhesive pads 130 may be formed by bending a portion of each of the risers 124 at a distal end of the riser 124 , such as bending the distal end at an angle of approximately 90 degrees. As such, the adhesive pad 130 is substantially perpendicular to the rest of the riser 124 and substantially parallel to the backer sheet 120 .
- each of the adhesive pads 130 has a small aperture 132 to allow an adhesive or other bonding agent to pass through the aperture 132 to a side of the adhesive pad 130 opposite to the side on which the adhesive is applied and thereby form a mechanical attachment to both sides of the adhesive pad 130 (see, e.g., FIG. 6 ).
- FIGS. 13 and 14 another embodiment of a mini-truss thin-sheet panel assembly according to the present invention includes a backer 140 .
- the backer 140 includes a first backer sheet 141 and a second backer sheet 142 that are each substantially similar to the backer sheet 122 of the backer 120 described above.
- the first and second backer sheets 141 , 142 are stacked with a lower surface of the first backer sheet 141 resting on an upper surface of the second backer sheet 142 .
- the first backer sheet 141 includes a plurality of first risers 143 formed in rows, the first risers 143 extending away from and substantially perpendicular to the first backer sheet 141 , similar to the risers 124 of the backer 120 described above.
- the first risers 143 may be integrally formed from the first backer sheet 141 , such as cut from and bent away from the first backer sheet 141 at a bend line to form a corresponding plurality of first openings 144 in the first backer sheet 141 , similar to the backer 120 described above.
- each of the first risers 143 includes a first adhesive pad 145 that is formed by bending a distal end of each of the first risers 143 .
- the second backer sheet 142 similar to the first backer sheet 141 , includes a plurality of second risers 146 formed in rows, the second risers 146 extending away from and substantially perpendicular to the second backer sheet 142 .
- the second risers 146 may be integrally formed from the second backer sheet 142 , such as cut from and bent away from the second backer sheet 142 at a bend line to form a corresponding plurality of second openings 147 in the second backer sheet 142 .
- each of the second risers 146 includes a second adhesive pad 148 that is formed by bending a distal end of each of the second risers 146 .
- Each of the second adhesive pads 148 , and also the first adhesive pads 145 may include an aperture 149 , similar to the apertures 132 of the backer 120 described above, for allowing an adhesive to spread to an opposite surface of each of the first and second adhesive pads 145 , 148 .
- the first backer sheet 141 rests on the second backer sheet 142 .
- each of the second risers 146 of the second backer sheet 142 extends through one of the first openings 144 of the first backer sheet 141 .
- the first and second backer sheets 141 , 142 are oriented relative to one another such that the planes of the first risers 143 are substantially perpendicular to the planes of the second risers 146 . That is, the rows of the first risers 143 run substantially perpendicularly to the rows of the second risers 146 .
- Such a configuration of the first and second risers 143 , 146 provides the backer 140 with stiffness in two directions.
- Both the first risers 143 and the second risers 146 are attached to a thin sheet at the first and second adhesive pads 145 , 148 , such as via an adhesive.
- a backer 150 may include a backer having any suitable configuration for maintaining the thin sheet 110 in a rigid or substantially rigid configuration and having a desired curvature.
- a backer 150 includes a backer sheet 152 having a plurality of risers 154 .
- the risers 154 also have triangular-shaped configurations, but differ from the risers 124 of the backer 120 in that the risers 154 have distal ends that terminate as corners of the triangular configurations, rather than having a protruding feature, such as the adhesive pads 130 of the risers 124 .
- the risers 154 may be staggered, for example, rather than arranged in regularly spaced rows and columns.
- another backer 160 includes a backer sheet 162 having a plurality of risers 164 .
- the risers 164 also have triangular-shaped configurations. However, distal ends of the risers 164 point in opposite directions in alternating rows.
- a backer 170 includes a backer sheet 172 having a plurality of risers 174 .
- the risers 174 also have triangular-shaped configurations, but the triangular-shaped risers 174 are arranged at substantially right angles to one another in alternating rows. That is, fold lines of rows of a first group of the risers 174 are substantially perpendicular to fold lines of rows of a second group of the risers 174 .
- first group of the risers 174 will extend from the backer sheet 172 in first group planes
- second group of the risers 174 will extend from the backer sheet 172 in second group planes, the second group planes being substantially perpendicular to the first group planes.
- the risers 174 of the backer 170 will provide rigidity to the mini-truss thin-sheet panel assembly in two directions.
- a backer 180 includes a backer sheet 182 having a plurality of risers 184 extending away from the backer sheet.
- the risers 184 differ from the previously described embodiments in that the risers 184 have rectangular-shaped configurations.
- a backer of a mini-truss thin-sheet panel assembly may include any suitable combination of arrangements (e.g., radial or circular), shapes, sizes, and/or orientations of the risers, such as a combination of the riser configurations of the backers 120 , 150 , 160 , 170 , 180 , as described above.
- a mini-truss thin-sheet panel assembly according to the present invention may include risers having different heights from one another.
- a thin sheet can be supported to have a desired curvature, and a backer sheet from which the risers of varying heights extend could have a substantially flat curvature.
- a backer 190 may include riser elements 194 formed by pressing a backer sheet 192 between two tooling plates having protrusions (e.g., similar to the protrusions of a waffle iron) so as to form corresponding protrusions that are the riser elements 194 in the backer sheet 192 .
- the riser elements 194 may be configured to provide stiffness to the backer 190 (and also to the mini-truss thin-sheet panel assembly) in two directions.
- riser elements may include triangles or other shapes separated and bent away from a backer sheet, as described above with respect to the backer 120 , but the riser elements may instead be grouped and the distal ends bent toward one another, such as by bending three or four triangular-shaped risers to form a pyramid-shaped configuration.
- a thin sheet may be attached to the distal ends of the riser elements that form the top of the pyramid.
- a mini-truss thin-sheet panel assembly may include a backer that is formed of various elements that are not integral to one another, but rather are combined by fasteners, adhesive, or any other suitable device. That is, unlike the backers 120 , 150 , 160 , 170 , 180 , 190 described above, in which the risers are formed from portions of the backer sheet, other embodiments may include riser elements that are separate from a backer sheet until they are attached to the backer sheet, such as by an adhesive or fastener.
- a backer may include a fluted fiberglass panel forming risers (the diagonal elements of the mini-truss) and a separate flat panel forming the backer sheet (the lower chord of the mini-truss).
- the thin sheet 110 and the backer 120 are attached to one another via bonding, fusing, adhesives, fasteners, or any other suitable device or combination thereof.
- the thin sheet 110 and the backer 120 are adhered to one another utilizing an adhesive 135 .
- the adhesive 135 may be an epoxy adhesive, or alternatively, may be any other suitable adhesive material.
- the adhesive 135 is applied to the adhesive pads 130 of the backer 120 .
- the apertures 132 of the adhesive pads 130 allow the adhesive 135 to spread to each side of the adhesive pads 130 , thereby providing a stronger adhesion of the thin sheet 110 and the backer 120 to one another.
- a computer numerical controlled (CNC) machine may be utilized to apply the adhesive 135 in selected regions (e.g., the adhesive pads 130 ) of the backer 120 .
- CNC computer numerical controlled
- the adhesive 135 may be applied more quickly and positioned more accurately, for example.
- the adhesive 135 may be cured or otherwise set to an adhering state, or cured more quickly, by putting the mini-truss thin-sheet panel assembly 100 in an oven or other temperature-controlling device for any suitable period of time until the thin sheet 110 and the backer 120 are adequately (e.g., permanently) adhered to one another.
- a bonding fixture 200 for shaping a mini-truss thin-sheet panel assembly to have a selected curvature includes a first portion 202 (e.g., a lower half) (see FIG. 23 ) and a second portion 204 (e.g., an upper half) (see FIG. 24 ).
- the first portion 202 has a first contoured surface 206 (e.g., a top surface), and the second portion 204 has a second contoured surface 208 (e.g., a bottom surface) that is substantially the same but facing opposite the first contoured surface 206 . That is, the first and second contoured surfaces 206 , 208 have substantially similar radii of curvature, but one (e.g., the first contoured surface 206 ) is concave and the other (e.g., the second contoured surface 208 ) is convex such that the first and second contoured surfaces 206 , 208 are substantially equally spaced from one another throughout.
- the bonding fixture 200 includes fasteners, or a clamp, vice, or any other suitable device or apparatus, for clamping or drawing the first and second portions 202 , 204 toward one another with a mini-truss thin-sheet panel assembly (e.g., the mini-truss thin-sheet panel assembly 100 ) sandwiched therebetween, as shown in FIG. 27 .
- the bonding fixture 200 includes bolts 210 , washers 211 , and wing nuts 212 for clamping the first and second portions 202 , 204 against the mini-truss thin-sheet panel assembly.
- the first portion 202 of the bonding fixture 200 includes a first panel 216 having the first contoured surface 206 (e.g., an upper surface of the first panel 216 ).
- the second portion 204 of the bonding fixture 200 includes a second panel 218 having the second contoured surface 208 (e.g., a lower surface of the second panel 218 ).
- the first and second portions 202 , 204 may include ribs 214 for supporting the first and second panels 216 and 218 and producing the desired curvatures of the first and second contoured surfaces 206 , 208 .
- Attachment of the thin sheet 110 and the backer 120 to one another, as well as shaping the mini-truss thin-sheet panel assembly 100 to have a selected curvature, may be facilitated utilizing the bonding fixture 200 .
- the first and second contours 206 , 208 of the respective first and second portions 202 , 204 of the bonding fixture 200 conform to the geometric shape or curvature that the mini-truss thin-sheet panel assembly 100 is desired to exhibit.
- the first and second portions 202 , 204 of the bonding fixture 200 are separated (see FIG. 25 ) by loosening the wing nuts 212 from the bolts 210 , or by opening any alternative clamping or fastening device.
- the backer 120 is placed on the first portion 202 of the bonding fixture 200 .
- the adhesive 135 or any other suitable bonding agent, is applied to the adhesive pads 130 of the risers 124 .
- the thin sheet 110 is positioned on the risers 124 of the backer 120 .
- the mini-truss thin-sheet panel assembly 100 is not yet shaped to have a selected curvature (see FIG. 26 ).
- the adhesive 135 may be applied to the adhesive pads 130 and the thin sheet 110 positioned on the risers 124 of the backer 120 prior to placing the backer 120 on the first portion 202 of the bonding fixture 200 .
- the second portion 204 of the bonding fixture is drawn toward the first portion 202 and tightened against the mini-truss thin-sheet panel assembly 100 by tightening the wing nuts 212 (or by clamping any alternative clamping or tightening device) of the bonding fixture 200 (see FIG. 27 ).
- the mini-truss thin-sheet panel assembly 100 retains the curvature or contour of the first and second contoured surfaces 206 , 208 of the respective first and second portions 202 , 204 of the bonding fixture 200 .
- mini-truss thin-sheet panel assembly as applied to a solar collector trough
- novel aspects of the mini-truss thin-sheet panel assembly of the invention may also be carried out by utilizing alternative structures, sizes, shapes, and/or materials in embodiments of the mini-truss thin-sheet panel assembly of the present invention.
- a thin panel which has been described above with respect to the mini-truss thin-sheet panel assembly 100 as the thin sheet 110 , may not be reflective, but rather, may be formed of an alternative material for purposes of decoration, strength, or otherwise.
- Embodiments of the mini-truss thin-sheet panel assembly may, for example, be applied to any market sector, such as, but not limited to, solar power generation, science, structural or decorative architecture, and industry.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Optical Elements Other Than Lenses (AREA)
- Laminated Bodies (AREA)
- Photovoltaic Devices (AREA)
- Assembled Shelves (AREA)
- Forms Removed On Construction Sites Or Auxiliary Members Thereof (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/254,795 US8327604B2 (en) | 2007-10-18 | 2008-10-20 | Mini-truss thin-sheet panel assembly |
US13/709,384 US8607529B2 (en) | 2007-10-18 | 2012-12-10 | Mini-truss thin-sheet panel assembly |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US99983307P | 2007-10-18 | 2007-10-18 | |
US12/254,795 US8327604B2 (en) | 2007-10-18 | 2008-10-20 | Mini-truss thin-sheet panel assembly |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/709,384 Continuation US8607529B2 (en) | 2007-10-18 | 2012-12-10 | Mini-truss thin-sheet panel assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
US20090101195A1 US20090101195A1 (en) | 2009-04-23 |
US8327604B2 true US8327604B2 (en) | 2012-12-11 |
Family
ID=40562235
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/254,795 Expired - Fee Related US8327604B2 (en) | 2007-10-18 | 2008-10-20 | Mini-truss thin-sheet panel assembly |
US13/709,384 Expired - Fee Related US8607529B2 (en) | 2007-10-18 | 2012-12-10 | Mini-truss thin-sheet panel assembly |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/709,384 Expired - Fee Related US8607529B2 (en) | 2007-10-18 | 2012-12-10 | Mini-truss thin-sheet panel assembly |
Country Status (9)
Country | Link |
---|---|
US (2) | US8327604B2 (ar) |
EP (1) | EP2201192A4 (ar) |
CN (1) | CN102216543B (ar) |
AU (1) | AU2008311746B2 (ar) |
EG (1) | EG26440A (ar) |
IL (1) | IL205164A (ar) |
MA (1) | MA31887B1 (ar) |
WO (1) | WO2009052520A1 (ar) |
ZA (1) | ZA201002839B (ar) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8607529B2 (en) * | 2007-10-18 | 2013-12-17 | Gossamer Space Frames | Mini-truss thin-sheet panel assembly |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU2009268667A1 (en) * | 2008-07-09 | 2010-01-14 | Skyfuel, Inc. | Solar collectors having slidably removable reflective panels for use in solar thermal applications |
US8739492B2 (en) * | 2008-07-09 | 2014-06-03 | Skyfuel, Inc. | Space frame connector |
WO2010022280A1 (en) | 2008-08-22 | 2010-02-25 | Skyfuel, Inc. | Hydraulic-based rotational system for solar concentrators that resists high wind loads without a mechanical lock |
US8627632B2 (en) | 2008-08-29 | 2014-01-14 | Werner Extrusion Solutions LLC | Node, apparatus, system and method regarding a frame support for solar mirrors |
US8887470B2 (en) | 2008-08-29 | 2014-11-18 | Werner Extrusion Solutions LLC | Solar trough frame, part and method |
DE202008016704U1 (de) * | 2008-12-18 | 2009-03-12 | Sk Energy Gmbh | Solarmodul und Solaranlage |
US8322333B2 (en) * | 2009-04-01 | 2012-12-04 | Abengoa Solar Inc. | Torque transfer between trough collector modules |
US8615960B2 (en) | 2009-07-24 | 2013-12-31 | Abengoa Solar Inc. | Solar collector module |
US11988415B2 (en) * | 2009-08-26 | 2024-05-21 | Werner Extrusion Solutions, Llc | Solar mirror array system, methods and apparatuses thereto |
US9184321B2 (en) | 2009-09-02 | 2015-11-10 | 3M Innovative Properties Company | Concentrating solar mirror panel assembly with corrugated stiffener |
US8132391B2 (en) * | 2009-10-23 | 2012-03-13 | Gossamer Space Frames | Thin mirror with truss backing and mounting arrangement therefor |
DE102010022423A1 (de) * | 2010-06-01 | 2011-12-01 | 3A Technology & Management Ag | Sonnenlichtreflektor für ein Solarkraftwerk |
WO2011157799A1 (en) * | 2010-06-16 | 2011-12-22 | Siemens Aktiengesellschaft | Solar collector assembly with at least one clinching connection, method for manufacturing the solar collector assembly by a clinching mechanism and use of the solar collector assembly |
US8039777B2 (en) * | 2010-07-08 | 2011-10-18 | Skyline Solar, Inc. | Solar collector with reflector having compound curvature |
WO2012061211A2 (en) | 2010-11-02 | 2012-05-10 | 3M Innovative Properties Company | Reflective articles and methods of making the same |
MX2013013729A (es) * | 2011-05-24 | 2014-02-27 | Magna Int Inc | Montaje de estructura de soporte y metodo para conformar un montaje de estructura de soporte. |
WO2013133859A1 (en) * | 2011-06-07 | 2013-09-12 | Salflex Polymers Limited | Hollow article with internal structural members |
FR2976846B1 (fr) * | 2011-06-23 | 2013-07-05 | Frederic Brun | Ame de materiau structural feuille et procede d'assemblage |
WO2013033329A1 (en) * | 2011-09-02 | 2013-03-07 | Werner Extrusion Solutions LLC | Solar mirror array system, methods and apparatuses thereto |
EP2809509A4 (en) | 2012-01-31 | 2015-09-23 | 3M Innovative Properties Co | METHOD FOR BORDER SEALING OF MULTILAYER ARTICLES |
EP2631556A1 (en) * | 2012-02-21 | 2013-08-28 | Areva Solar, Inc | Reflector panel for solar power plant, reflector assembly comprising such a panel, and related manufacturing method |
EP2844469A1 (en) | 2012-05-03 | 2015-03-11 | 3M Innovative Properties Company | Durable solar mirror films |
EP2844464A4 (en) | 2012-05-03 | 2015-12-23 | 3M Innovative Properties Co | DURABLE SOLAR MIRROR FILMS |
FR2990430B1 (fr) * | 2012-05-14 | 2018-05-18 | Helioclim | Procede de mise en forme d'une feuille de verre et miroir comportant une telle feuille de verre |
KR101534971B1 (ko) * | 2013-12-19 | 2015-07-07 | 현대자동차주식회사 | 자동차용 염료감응 태양전지의 곡면화 방법 |
WO2017196188A1 (en) * | 2016-05-09 | 2017-11-16 | Insolare Group Limited | Improvements to concentrating solar power systems, components therefore, and methods of manufacture and assembly |
US9874006B1 (en) * | 2016-08-01 | 2018-01-23 | Inhabit Solar, Llc | Modular roof mounting system |
US10829932B2 (en) | 2018-09-08 | 2020-11-10 | Paul Winton Wennberg | Shapeable bundles of slidably-interlocked extrusions for architectural or other construction components |
CN114046608B (zh) * | 2021-10-25 | 2024-06-04 | 中国电建集团西北勘测设计研究院有限公司 | 一种定日镜多点面形自动调节系统及装配方法 |
Citations (71)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US963889A (en) | 1909-08-14 | 1910-07-12 | John B Goodwin | Sheet-metal building construction. |
US1433232A (en) | 1920-11-17 | 1922-10-24 | Rogers Richard Hawke | Beam or like structural member for use in reenforced concrete construction and other purposes |
US1576559A (en) * | 1925-08-03 | 1926-03-16 | Swift Joseph Kay | Structural material |
DE609681C (de) | 1935-03-23 | Ernst Landolt | Aus gepraegter Pappe o. dgl. bestehendes Packmaterial | |
US2391997A (en) | 1942-03-26 | 1946-01-01 | Lilly Florence Shirley Noble | Composite slab sheet or plate |
US2792164A (en) | 1951-08-10 | 1957-05-14 | Cauffiel John | Preformed structural units |
US2990038A (en) | 1959-05-29 | 1961-06-27 | Diamond Harry | Structural beams |
US3008551A (en) * | 1958-05-29 | 1961-11-14 | Dana Corp | Structural panel construction |
US3046638A (en) | 1958-02-17 | 1962-07-31 | Jean H Melzer | Method of producing hollow sheetmetal panel structures |
US3050831A (en) | 1959-05-29 | 1962-08-28 | Diamond Harry | Methods of making structural beams |
US3111204A (en) | 1959-08-24 | 1963-11-19 | British Uralite Ltd | Structural element and a method of making a structural element |
US3266790A (en) | 1961-07-14 | 1966-08-16 | Roger G Bradeen | Cushioning media |
US3380217A (en) | 1965-07-15 | 1968-04-30 | Nat Lead Co | Raised floor plate |
US3392500A (en) | 1961-08-11 | 1968-07-16 | Johnston Charles Richard | Freight car construction |
US3415027A (en) | 1965-07-30 | 1968-12-10 | Butler Manufacturing Co | Truss of spaced pyramidal units |
US3507634A (en) * | 1965-10-22 | 1970-04-21 | United Aircraft Corp | Composite metal structure |
US3525663A (en) | 1967-03-09 | 1970-08-25 | Jesse R Hale | Anticlastic cellular core structure having biaxial rectilinear truss patterns |
US3673057A (en) * | 1970-07-22 | 1972-06-27 | Fmc Corp | Cellular structures |
US3793791A (en) * | 1971-10-21 | 1974-02-26 | W Wootten | Method and apparatus for forming a panel for use as a structural element |
US3834487A (en) | 1973-03-08 | 1974-09-10 | J Hale | Sandwich core panel with structural decoupling between the outer face sheets thereof |
US3938963A (en) | 1973-10-01 | 1976-02-17 | Hale Jesse R | Sandwich core panel having cured face sheets and a core formed with projecting modes |
US3940811A (en) | 1972-07-17 | 1976-03-02 | Idemitsu, Kosan Kabushiki-Kaisha (Idemitsu Kosan Co., Ltd.) | Lightweight construction materials and articles made thereof |
DE2558612A1 (de) | 1975-12-24 | 1977-07-07 | Zink Walter | Transparente kunststoffplatte |
US4087302A (en) | 1975-07-23 | 1978-05-02 | Wootten William A | Method for forming a structural panel |
US4139670A (en) * | 1975-11-24 | 1979-02-13 | Loewe Anstalt | Composite panel material with metal skeleton |
US4181556A (en) * | 1975-11-24 | 1980-01-01 | Loewe Anstalt | Composite panel materials and method of manufacture |
US4203268A (en) | 1978-03-13 | 1980-05-20 | Tate Architectural Products, Inc. | Structural member and composite panel including same |
GB1577453A (en) | 1976-11-15 | 1980-10-22 | Pirelli | Solar energy panel |
US4276873A (en) | 1979-06-25 | 1981-07-07 | Alpha Solarco Inc. | Reflectors for solar energy collectors |
US4411121A (en) | 1981-02-02 | 1983-10-25 | Tate Architectural Products, Inc. | Structural member with truncated conical portion and composite panel including same |
US4426824A (en) | 1981-05-18 | 1984-01-24 | Donn Incorporated | Floor panel and method of making same |
US4435043A (en) | 1981-08-21 | 1984-03-06 | Glaverbel | Composite mirror panels |
US4571812A (en) | 1984-02-16 | 1986-02-25 | Industrial Solar Technology | Method for making a solar concentrator and product |
US4599771A (en) | 1985-02-21 | 1986-07-15 | Texas Instruments Incorporated | Method of making a stiffened composite metal panel |
US4607616A (en) | 1982-02-16 | 1986-08-26 | Klaus Lehmann | Roof cladding or similar building element allowing heat exchange with the environment and usable particularly as a solar energy collector |
FR2621677A1 (fr) | 1987-10-13 | 1989-04-14 | Heuliez Henri France Design | Structure rigide destinee a la realisation de panneaux ou d'elements tridimensionnels |
FR2630478A2 (fr) | 1988-02-02 | 1989-10-27 | Boudet Pierre | Panneau pliant notamment pour la realisation de cloisons |
US4967533A (en) * | 1988-11-02 | 1990-11-06 | Tetrahex, Inc. | Tetrahexagonal truss structure |
US4973506A (en) * | 1987-10-30 | 1990-11-27 | Ciba-Geigy Ag | Composite plate for the facing of building surfaces |
US5005800A (en) * | 1988-11-02 | 1991-04-09 | Tetrahex, Inc. | Die for making a tetrahexagonal truss structure |
DE9103890U1 (de) | 1991-03-27 | 1991-08-01 | Schubert, Frank Werner, O-6401 Theuern | Optiminierter Vakuum-Flachkollektor |
US5040966A (en) * | 1988-11-02 | 1991-08-20 | Tetrahex, Inc. | Die for making a tetrahexagonal truss structure |
WO1993004240A1 (en) | 1991-08-14 | 1993-03-04 | Ralph Warwick Skoien | Reflective insulation batts |
DE4221752A1 (de) | 1992-07-02 | 1994-01-05 | Werner Dipl Ing Meinhardt | Bauplatte |
WO1997008404A1 (en) | 1995-08-28 | 1997-03-06 | Jensen, Per, Harald | A space element |
DE19610022A1 (de) | 1996-03-14 | 1997-09-18 | Univ Dresden Tech | Mehrschichtiges Leichtbauelement und Herstellungsverfahren |
US5768851A (en) | 1997-03-26 | 1998-06-23 | Nagaoka; Tadayoshi | Structure unit |
US5809737A (en) | 1994-12-16 | 1998-09-22 | British Aerospace Plc | Structural parts for use in aircraft |
US5979139A (en) | 1998-01-06 | 1999-11-09 | Aero Transportation Products, Inc. | Lightweight, self-supporting paneling |
US6036323A (en) | 1996-12-18 | 2000-03-14 | Products Innovation Center, Inc. | Solar insolation concentrator, fabrication tool and fabrication process |
FR2786746A1 (fr) | 1998-12-02 | 2000-06-09 | Lorraine Laminage | Flan metallique multicouche et procede de fabrication d'un tel flan metallique multicouche |
US6167671B1 (en) * | 1998-12-21 | 2001-01-02 | Steven D. Wilson | Prefabricated concrete wall form system |
US6200664B1 (en) | 1999-11-01 | 2001-03-13 | Ward Figge | Explosion barrier |
US6207256B1 (en) * | 1997-10-02 | 2001-03-27 | S. Iwasa | Space truss composite panel |
US20010036024A1 (en) | 2000-05-05 | 2001-11-01 | Doug Wood | Matrix solar dish |
WO2001094710A1 (en) | 2000-06-06 | 2001-12-13 | Kuchel, Karin | Prefabricated collapsible panel for walls, floors, ceilings and rooves |
US20020020134A1 (en) | 2000-08-08 | 2002-02-21 | Collard Richard W. | Building truss structure |
US6644535B2 (en) | 2001-05-18 | 2003-11-11 | Massachusetts Institute Of Technology | Truss core sandwich panels and methods for making same |
US20040168383A1 (en) | 2002-03-01 | 2004-09-02 | Reynolds Glenn A. | Method and apparatus for cladding elongated structural members |
US20040216734A1 (en) | 2001-05-29 | 2004-11-04 | Paul Lawheed | Conversion of solar energy |
US20050126106A1 (en) | 2003-12-12 | 2005-06-16 | Murphy David M. | Deployable truss having second order augmentation |
US20050183376A1 (en) | 2003-09-01 | 2005-08-25 | Bunichi Shoji | Space truss structure surface slab assembly |
US6939599B2 (en) * | 1996-09-13 | 2005-09-06 | Brian H. Clark | Structural dimple panel |
US20070011983A1 (en) | 2004-08-31 | 2007-01-18 | Reynolds Glenn A | Space frames and connection node arrangement for them |
US20070020441A1 (en) | 2005-07-22 | 2007-01-25 | Hongseong Industrial Co., Ltd | Core for a sandwich panel manufactured by deep drawing and a sandwich panel thereby |
US20070169432A1 (en) | 2003-12-03 | 2007-07-26 | Bridge Iain N | Panel structure |
US7288326B2 (en) | 2002-05-30 | 2007-10-30 | University Of Virginia Patent Foundation | Active energy absorbing cellular metals and method of manufacturing and using the same |
US7424967B2 (en) | 2002-09-03 | 2008-09-16 | University Of Virginia Patent Foundation | Method for manufacture of truss core sandwich structures and related structures thereof |
FI20070691A (fi) * | 2007-09-11 | 2009-03-12 | Outokumpu Oy | Paneelirakenne |
US7614201B2 (en) | 2005-10-04 | 2009-11-10 | Federal-Mogul World Wide, Inc. | Sheet metal joint |
US7736721B2 (en) | 2006-08-10 | 2010-06-15 | International Automotive Components Group North America, Inc. | Hollow structural member with reinforced bulwark and process for producing same |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4124277A (en) * | 1977-02-16 | 1978-11-07 | Martin Marietta Corporation | Parabolic mirror construction |
US4238265A (en) * | 1978-10-27 | 1980-12-09 | The Boeing Company | Method of manufacturing a glass parabolic-cylindrical solar collector |
US4373783A (en) * | 1980-04-07 | 1983-02-15 | Atlantic Richfield Company | Thermally stabilized heliostat |
GB2112513B (en) * | 1981-12-23 | 1985-07-03 | Parly Tools Manufacturing Limi | Combined fluorescent lamp and spotlight |
JPS61125840A (ja) * | 1984-11-26 | 1986-06-13 | トステム株式会社 | サンドイツチパネル用コア |
US5162143A (en) | 1990-03-30 | 1992-11-10 | The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration | Core design for use with precision composite reflectors |
US5424113A (en) * | 1993-06-23 | 1995-06-13 | The United States Of America As Represented By The Secretary Of The Navy | Lattice core sandwich construction |
US5543204A (en) * | 1995-01-05 | 1996-08-06 | The United States Of America As Represented By The Secretary Of The Navy | Bi-directionally corrugated sandwich construction |
US5609942A (en) * | 1995-03-13 | 1997-03-11 | The United States Of America As Represented By The Secretary Of The Navy | Panel having cross-corrugated sandwich construction |
JPH0970907A (ja) * | 1995-09-06 | 1997-03-18 | Oyo Kikaku:Kk | コアー材と複合盤体 |
US5894045A (en) * | 1996-11-12 | 1999-04-13 | Desrondiers; Bernard R. | Cellular core structure building component |
CN102216543B (zh) * | 2007-10-18 | 2014-08-27 | 游丝空间框架公司 | 微型桁架薄片面板组件 |
WO2009108712A2 (en) * | 2008-02-26 | 2009-09-03 | Klaus Stadthagen-Gonzalez | Structural element |
-
2008
- 2008-10-20 CN CN200880114384.2A patent/CN102216543B/zh not_active Expired - Fee Related
- 2008-10-20 US US12/254,795 patent/US8327604B2/en not_active Expired - Fee Related
- 2008-10-20 WO PCT/US2008/080550 patent/WO2009052520A1/en active Application Filing
- 2008-10-20 EP EP08839792.2A patent/EP2201192A4/en not_active Withdrawn
- 2008-10-20 AU AU2008311746A patent/AU2008311746B2/en not_active Ceased
-
2010
- 2010-04-18 EG EG2010040620A patent/EG26440A/ar active
- 2010-04-18 IL IL205164A patent/IL205164A/en not_active IP Right Cessation
- 2010-04-22 ZA ZA2010/02839A patent/ZA201002839B/en unknown
- 2010-05-10 MA MA32828A patent/MA31887B1/ar unknown
-
2012
- 2012-12-10 US US13/709,384 patent/US8607529B2/en not_active Expired - Fee Related
Patent Citations (75)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE609681C (de) | 1935-03-23 | Ernst Landolt | Aus gepraegter Pappe o. dgl. bestehendes Packmaterial | |
US963889A (en) | 1909-08-14 | 1910-07-12 | John B Goodwin | Sheet-metal building construction. |
US1433232A (en) | 1920-11-17 | 1922-10-24 | Rogers Richard Hawke | Beam or like structural member for use in reenforced concrete construction and other purposes |
US1576559A (en) * | 1925-08-03 | 1926-03-16 | Swift Joseph Kay | Structural material |
US2391997A (en) | 1942-03-26 | 1946-01-01 | Lilly Florence Shirley Noble | Composite slab sheet or plate |
US2792164A (en) | 1951-08-10 | 1957-05-14 | Cauffiel John | Preformed structural units |
US3046638A (en) | 1958-02-17 | 1962-07-31 | Jean H Melzer | Method of producing hollow sheetmetal panel structures |
US3008551A (en) * | 1958-05-29 | 1961-11-14 | Dana Corp | Structural panel construction |
US2990038A (en) | 1959-05-29 | 1961-06-27 | Diamond Harry | Structural beams |
US3050831A (en) | 1959-05-29 | 1962-08-28 | Diamond Harry | Methods of making structural beams |
US3111204A (en) | 1959-08-24 | 1963-11-19 | British Uralite Ltd | Structural element and a method of making a structural element |
US3266790A (en) | 1961-07-14 | 1966-08-16 | Roger G Bradeen | Cushioning media |
US3392500A (en) | 1961-08-11 | 1968-07-16 | Johnston Charles Richard | Freight car construction |
US3380217A (en) | 1965-07-15 | 1968-04-30 | Nat Lead Co | Raised floor plate |
US3415027A (en) | 1965-07-30 | 1968-12-10 | Butler Manufacturing Co | Truss of spaced pyramidal units |
US3507634A (en) * | 1965-10-22 | 1970-04-21 | United Aircraft Corp | Composite metal structure |
US3525663A (en) | 1967-03-09 | 1970-08-25 | Jesse R Hale | Anticlastic cellular core structure having biaxial rectilinear truss patterns |
US3673057A (en) * | 1970-07-22 | 1972-06-27 | Fmc Corp | Cellular structures |
US3793791A (en) * | 1971-10-21 | 1974-02-26 | W Wootten | Method and apparatus for forming a panel for use as a structural element |
US3940811A (en) | 1972-07-17 | 1976-03-02 | Idemitsu, Kosan Kabushiki-Kaisha (Idemitsu Kosan Co., Ltd.) | Lightweight construction materials and articles made thereof |
US3834487A (en) | 1973-03-08 | 1974-09-10 | J Hale | Sandwich core panel with structural decoupling between the outer face sheets thereof |
US3938963A (en) | 1973-10-01 | 1976-02-17 | Hale Jesse R | Sandwich core panel having cured face sheets and a core formed with projecting modes |
US4087302A (en) | 1975-07-23 | 1978-05-02 | Wootten William A | Method for forming a structural panel |
US4139670A (en) * | 1975-11-24 | 1979-02-13 | Loewe Anstalt | Composite panel material with metal skeleton |
US4181556A (en) * | 1975-11-24 | 1980-01-01 | Loewe Anstalt | Composite panel materials and method of manufacture |
DE2558612A1 (de) | 1975-12-24 | 1977-07-07 | Zink Walter | Transparente kunststoffplatte |
GB1577453A (en) | 1976-11-15 | 1980-10-22 | Pirelli | Solar energy panel |
US4203268A (en) | 1978-03-13 | 1980-05-20 | Tate Architectural Products, Inc. | Structural member and composite panel including same |
US4276873A (en) | 1979-06-25 | 1981-07-07 | Alpha Solarco Inc. | Reflectors for solar energy collectors |
US4411121A (en) | 1981-02-02 | 1983-10-25 | Tate Architectural Products, Inc. | Structural member with truncated conical portion and composite panel including same |
US4426824A (en) | 1981-05-18 | 1984-01-24 | Donn Incorporated | Floor panel and method of making same |
US4435043A (en) | 1981-08-21 | 1984-03-06 | Glaverbel | Composite mirror panels |
US4607616A (en) | 1982-02-16 | 1986-08-26 | Klaus Lehmann | Roof cladding or similar building element allowing heat exchange with the environment and usable particularly as a solar energy collector |
US4571812A (en) | 1984-02-16 | 1986-02-25 | Industrial Solar Technology | Method for making a solar concentrator and product |
US4599771A (en) | 1985-02-21 | 1986-07-15 | Texas Instruments Incorporated | Method of making a stiffened composite metal panel |
FR2621677A1 (fr) | 1987-10-13 | 1989-04-14 | Heuliez Henri France Design | Structure rigide destinee a la realisation de panneaux ou d'elements tridimensionnels |
US4973506A (en) * | 1987-10-30 | 1990-11-27 | Ciba-Geigy Ag | Composite plate for the facing of building surfaces |
FR2630478A2 (fr) | 1988-02-02 | 1989-10-27 | Boudet Pierre | Panneau pliant notamment pour la realisation de cloisons |
US5005800A (en) * | 1988-11-02 | 1991-04-09 | Tetrahex, Inc. | Die for making a tetrahexagonal truss structure |
US5040966A (en) * | 1988-11-02 | 1991-08-20 | Tetrahex, Inc. | Die for making a tetrahexagonal truss structure |
US4967533A (en) * | 1988-11-02 | 1990-11-06 | Tetrahex, Inc. | Tetrahexagonal truss structure |
DE9103890U1 (de) | 1991-03-27 | 1991-08-01 | Schubert, Frank Werner, O-6401 Theuern | Optiminierter Vakuum-Flachkollektor |
WO1993004240A1 (en) | 1991-08-14 | 1993-03-04 | Ralph Warwick Skoien | Reflective insulation batts |
DE4221752A1 (de) | 1992-07-02 | 1994-01-05 | Werner Dipl Ing Meinhardt | Bauplatte |
US5809737A (en) | 1994-12-16 | 1998-09-22 | British Aerospace Plc | Structural parts for use in aircraft |
WO1997008404A1 (en) | 1995-08-28 | 1997-03-06 | Jensen, Per, Harald | A space element |
DE19610022A1 (de) | 1996-03-14 | 1997-09-18 | Univ Dresden Tech | Mehrschichtiges Leichtbauelement und Herstellungsverfahren |
US6939599B2 (en) * | 1996-09-13 | 2005-09-06 | Brian H. Clark | Structural dimple panel |
US6036323A (en) | 1996-12-18 | 2000-03-14 | Products Innovation Center, Inc. | Solar insolation concentrator, fabrication tool and fabrication process |
US5768851A (en) | 1997-03-26 | 1998-06-23 | Nagaoka; Tadayoshi | Structure unit |
US6207256B1 (en) * | 1997-10-02 | 2001-03-27 | S. Iwasa | Space truss composite panel |
US5979139A (en) | 1998-01-06 | 1999-11-09 | Aero Transportation Products, Inc. | Lightweight, self-supporting paneling |
FR2786746A1 (fr) | 1998-12-02 | 2000-06-09 | Lorraine Laminage | Flan metallique multicouche et procede de fabrication d'un tel flan metallique multicouche |
US6167671B1 (en) * | 1998-12-21 | 2001-01-02 | Steven D. Wilson | Prefabricated concrete wall form system |
US6200664B1 (en) | 1999-11-01 | 2001-03-13 | Ward Figge | Explosion barrier |
US20010036024A1 (en) | 2000-05-05 | 2001-11-01 | Doug Wood | Matrix solar dish |
WO2001094710A1 (en) | 2000-06-06 | 2001-12-13 | Kuchel, Karin | Prefabricated collapsible panel for walls, floors, ceilings and rooves |
US20020020134A1 (en) | 2000-08-08 | 2002-02-21 | Collard Richard W. | Building truss structure |
US6644535B2 (en) | 2001-05-18 | 2003-11-11 | Massachusetts Institute Of Technology | Truss core sandwich panels and methods for making same |
US20040216734A1 (en) | 2001-05-29 | 2004-11-04 | Paul Lawheed | Conversion of solar energy |
US20040168383A1 (en) | 2002-03-01 | 2004-09-02 | Reynolds Glenn A. | Method and apparatus for cladding elongated structural members |
US7288326B2 (en) | 2002-05-30 | 2007-10-30 | University Of Virginia Patent Foundation | Active energy absorbing cellular metals and method of manufacturing and using the same |
US7424967B2 (en) | 2002-09-03 | 2008-09-16 | University Of Virginia Patent Foundation | Method for manufacture of truss core sandwich structures and related structures thereof |
US20050183376A1 (en) | 2003-09-01 | 2005-08-25 | Bunichi Shoji | Space truss structure surface slab assembly |
US20080155931A1 (en) | 2003-09-01 | 2008-07-03 | Bunichi Shoji | Space truss structure surface slab assembly |
US20070169432A1 (en) | 2003-12-03 | 2007-07-26 | Bridge Iain N | Panel structure |
US20050126106A1 (en) | 2003-12-12 | 2005-06-16 | Murphy David M. | Deployable truss having second order augmentation |
US20070011983A1 (en) | 2004-08-31 | 2007-01-18 | Reynolds Glenn A | Space frames and connection node arrangement for them |
US20070020441A1 (en) | 2005-07-22 | 2007-01-25 | Hongseong Industrial Co., Ltd | Core for a sandwich panel manufactured by deep drawing and a sandwich panel thereby |
US7614201B2 (en) | 2005-10-04 | 2009-11-10 | Federal-Mogul World Wide, Inc. | Sheet metal joint |
US7736721B2 (en) | 2006-08-10 | 2010-06-15 | International Automotive Components Group North America, Inc. | Hollow structural member with reinforced bulwark and process for producing same |
FI20070691A (fi) * | 2007-09-11 | 2009-03-12 | Outokumpu Oy | Paneelirakenne |
WO2009034226A1 (en) | 2007-09-11 | 2009-03-19 | Outokumpu Oyj | Panel structure |
EP2188077A1 (en) * | 2007-09-11 | 2010-05-26 | Outokumpu Oyj | Panel structure |
US20100186336A1 (en) | 2007-09-11 | 2010-07-29 | Outokumpu Oyj | Panel structure |
Non-Patent Citations (3)
Title |
---|
International Search Report and Written Opinion dated Dec. 22, 2008 for International application No. PCT/US 08/080550, 10 sheets. |
International Search Report for International Application No. PCT/US2010/053856, filed Oct. 22, 2010, International Search Report dated Feb. 22, 2011 and mailed Mar. 17, 2011 (5 pgs.). |
Written Opinion of the International Searching Authority for International Application No. PCT/US2010/053856, filed Oct. 22, 2010, Written Opinion dated Feb. 22, 2011 and mailed Mar. 17, 2011 (5 pgs.). |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8607529B2 (en) * | 2007-10-18 | 2013-12-17 | Gossamer Space Frames | Mini-truss thin-sheet panel assembly |
Also Published As
Publication number | Publication date |
---|---|
ZA201002839B (en) | 2011-02-23 |
WO2009052520A1 (en) | 2009-04-23 |
IL205164A0 (en) | 2010-11-30 |
AU2008311746A1 (en) | 2009-04-23 |
EP2201192A1 (en) | 2010-06-30 |
MA31887B1 (ar) | 2010-12-01 |
US8607529B2 (en) | 2013-12-17 |
CN102216543B (zh) | 2014-08-27 |
CN102216543A (zh) | 2011-10-12 |
US20090101195A1 (en) | 2009-04-23 |
AU2008311746B2 (en) | 2012-11-15 |
EP2201192A4 (en) | 2014-01-08 |
US20130161471A1 (en) | 2013-06-27 |
EG26440A (ar) | 2013-10-31 |
IL205164A (en) | 2013-01-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8607529B2 (en) | Mini-truss thin-sheet panel assembly | |
US8132391B2 (en) | Thin mirror with truss backing and mounting arrangement therefor | |
US20080308094A1 (en) | Trough reflectors for solar energy collectors | |
US20060150967A1 (en) | Solar collector | |
US4611575A (en) | Parabolic trough solar reflector | |
US4435043A (en) | Composite mirror panels | |
US20140117190A1 (en) | Support Frame Assembly And Method Of Forming A Support Frame Assembly | |
US6739729B1 (en) | Composite backed prestressed mirror for solar facet | |
US20100154888A1 (en) | Solar Module and Solar Device | |
WO2015130808A1 (en) | Mirror collector for parabolic solar trough | |
WO2017184893A1 (en) | Mirror collector for parabolic solar trough | |
US7810940B2 (en) | Adjustable table for shaping a mirror | |
US20230008043A1 (en) | Heliostat frame and heliostat thereof, and heliostat field | |
WO2012151671A1 (en) | Support arm assembly | |
US20130240473A1 (en) | Uniform tension distribution mechanism for stretched membrane solar collectors | |
CN118836586A (en) | Mirror surface fixing frame and heliostat mechanism |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: GOSSAMER SPACE FRAMES, CALIFORNIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:REYNOLDS, GLENN ALAN;HACKBARTH, DEAN ROBERT;CURTIS, GARY NOBLE;REEL/FRAME:022398/0697;SIGNING DATES FROM 20090225 TO 20090227 Owner name: GOSSAMER SPACE FRAMES, CALIFORNIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:REYNOLDS, GLENN ALAN;HACKBARTH, DEAN ROBERT;CURTIS, GARY NOBLE;SIGNING DATES FROM 20090225 TO 20090227;REEL/FRAME:022398/0697 |
|
STCF | Information on status: patent grant |
Free format text: PATENTED CASE |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
FEPP | Fee payment procedure |
Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
LAPS | Lapse for failure to pay maintenance fees |
Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20201211 |